Discontinuous supersonic flow past an ablating wavy wall.
- 1 April 1969
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in AIAA Journal
- Vol. 7 (4) , 762-764
- https://doi.org/10.2514/3.5211
Abstract
No abstract availableThis publication has 1 reference indexed in Scilit:
- An Analytic Extension of the Shock-Expansion MethodJournal of the Aerospace Sciences, 1961